VOYAGER
Voyager LECP Data Analysis Handbook
Instrument Modeling Reports
by Sheela Shodhan
E.4 FDMOD1.CMN
************************************************************************** * THIS IS A .CMN FILE THAT IS INCLUDED IN THE ROUTINE FDMOD1.FOR * * * * PURPOSE : IT CONTAINS ALL THE PARAMETERS OF TRANSLATION, * * ROTATION,MAGNETISATION CONSTANTS A0,B0,MAGS THAT ARE * * USED TO DETERMINE THE MAGNETIC FIELD AT A POINT (X,Y,Z) * * IN SPACE DUE TO TWO TILTED MAGNETS. * * VARIABLES : * * A0,B0 : MAGNETISATION CONSTANTS. * * ANGLE : ANGLE IN DEGREES BY WHICH THE MAGNETS ARE TILTED. * * ANG : ANGLE IN RADIANS BY WHICH THE MAGNETS ARE TILTED. * * HALFD : HALF THE DISTANCE BETWEEN THE MAGNETS. * * LENGTHS : ARRAY THAT CONTAINS THE LENGTHS OF THE MAGNET PIECES. * * MAGS : 2-D ARRAY THAT CONTAINS THE MAGNETISATION OF THE MAGNET PIECES.* * MAX : MAXIMUM NUMBER OF PIECES OF THE MAGNET IN X AND Y DIRECTION. * * NX1,NY1 : NUMBER OF PIECES OF THE MAGNET IN X AND Y DIRECTION. * * SEPTS : ARRAY THAT CONTAINS THE DISTANCE BETWEEN THE CORRESPONDING * * PIECES OF THE TWO MAGNETS. * * WIDTHS : ARRAY THAT CONTAINS THE WIDTH OF THE MAGNET PIECES. * * X0,Y0 : CONSTANTS USED IN THE EXPRESSION OF THE LINEARLY FALLING * * MAGNETISATION : A(X-X0) + B(Y-Y0) * * XL,YL,ZL : CONSTANTS BY WHICH THE EXPERIMENTAL SYSTEM IS TRANSLATE * * -D WITH RESPECT TO THE COORDINATE SYSTEMS CENTRED AT THE MAGNETS. * ************************************************************************** INTEGER MAX,NX1,NY1 REAL*8 HALFD PARAMETER (HALFD=0.4375D0,MAX=15,NX1=1,NY1=1) REAL*8 ANGLE,ANG,PI,RAD,A0,B0,X0,Y0 REAL*8 XL(MAX),YL(MAX),ZL(MAX),LENGTHS(MAX),WIDTHS(MAX),SEPTS(MAX) REAL*8 MAGS(MAX,MAX)
PI = 4.0D0 * DATAN(1.0D0) RAD = 180.0D0/PI
DATA A0/0.75D0/,B0/3.5D0/,X0/0.0D0/,Y0/0.0D0/ DATA (LENGTHS(I),I=1,NX1)/0.4D0/ DATA (WIDTHS(I),I=1,NY1)/0.3D0/ DATA (XL(I),I=1,NX1)/0.0D0/ DATA (YL(I),I=1,NY1)/0.5D0/ DATA ZL(1)/0.43750D0/ DATA SEPTS(1)/0.8750D0/ DATA ANGLE/20.0D0/ ANG = ANGLE/RAD YL(1) = 0.5D0 * DCOS(ANG) DATA (MAGS(1,I),I=1,NY1)/1491.008264378091/
C------------------------------------------------------------------------- C-------------------------------------------------------------------------
Return to thesis table of contents.
Return to Voyager
LECP Data Analysis Handbook Table of Contents.
Return to Fundamental
Technologies Home Page.
Updated 8/9/19, Cameron Crane
VOYAGER 1 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
September 5, 1977, 12:56:00:00 UTC
*Since official launch
September 5, 1977, 12:56:00:00 UTC
VOYAGER 2 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
August 20, 1977, 14:29:00:00 UTC
*Since official launch
August 20, 1977, 14:29:00:00 UTC
QUICK FACTS
Manufacturer:
Voyagers 1 and 2 were built in the Jet Propulsion
Laboratory in Southern California.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.